Calculation of viscous effects on transonic flow for oscillating airfoils and comparisons with experiment /

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Bibliographic Details
Author / Creator:	Howlett, James T., author.
Imprint:	Washington, D.C. : National Aeronautics and Space Administration, Scientific and Technical Information Office, September 1987.
Description:	1 online resource (74 pages) : illustrations.
Language:	English
Series:	NASA/TP ; 2731 NASA technical paper ; 2731.
Subject:	Transonic flow. Viscous flow. Computational fluid dynamics. Airfoils. Oscillations. Aerodynamics, Transonic. Viscous flow. Unsteady flow (Aerodynamics) Oscillating wings (Aerodynamics) Boundary layer. Aerodynamics, Transonic. Boundary layer. Oscillating wings (Aerodynamics) Unsteady flow (Aerodynamics) Viscous flow.
Format:	E-Resource U.S. Federal Government Document Book
URL for this record:	http://pi.lib.uchicago.edu/1001/cat/bib/11665610

Hidden Bibliographic Details
Other authors / contributors:	Bland, Samuel R., author. United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch, issuing body. Langley Research Center.
Notes:	"September 1987." Prepared at Langley Research Center. Includes bibliographical references (page 13). Technical paper. Langley Research Center 505-63-21-01 L-16289 Description based on online resource, PDF version; title from title page (NASA, viewed July 20, 2018).
Other form:	Print version: Howlett, James T Calculation of viscous effects on transonic flow for oscillating airfoils and comparisons with experiment Microfiche : Howlett, James T Calculation of viscous effects on transonic flow for oscillating airfoils and comparisons with experiment
GPO item no.:	0830-H-15 (online)
Govt.docs classification:	NAS 1.60:2731

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